An aircraft comprises a fuselage and a wing, at least one hydrogen fuel tank and a fuel line configured to delivery fuel from the fuel tank to the engine. The fuel tank is installed externally of the fuselage and wing, and comprises an external aeroshell containing a plurality of pressure vessels configured to contain pressurised fuel therein.
Cryogenic fueled aircraft
17.05.2023
Patent
Elektronische Ressource
Englisch